Intel FALCON 8+ Flight Manual

DESCRIPTION
© 2017 Intel Corporation. All rights reserved. 83
REV 00
APR 2017
Manual-Mode
 When there is no input from the Remote Pilot, the system will only keep its orientation
in the air.
 The system will not keep its position and height, nor will it compensate for wind.
 Controlling the position and height has to be done manually by the Remote Pilot.
 The inputs via the Intel
®
Cockpit GCS control the roll and pitch angles and the thrust of
the Intel
®
Falcon™ 8+ UAS.
o Roll and pitch angles are limited to 50°.
o The direction and the speed of the Intel
®
Falcon™ 8+ UAS are influenced by the
wind direction and speed.
7.2.5 Camera Controls
All cameras integrated on the Intel
®
Falcon™ 8+ UAS can be controlled via the Intel
®
Cockpit GCS.
Several switches on the Intel
®
Cockpit GCS are assigned to camera controls.
1) Push Button #1 sets the camera to +/- 90° and 0° when R1 (4) is pushed simultaneously
2) Push Button #2 changes the function depending on the connected payload
3) Push Button $3 is the trigger button on top of the left control stick (control sick 1)
4) Left Rocker Switch, #4, controls the camera tilt
WARNING: MANUAL-MODE IS FOR EXPERTS ONLY.

Intel FALCON 8+ Specifications

General

Type	Octocopter
Easy to use	Yes
Product color	Black, Yellow
Maximum speed	16 m/s
Frequency band	2.4 GHz
Number of rotors	8 rotors
Maximum flight time	26 min
Maximum weight capacity	2.8 kg
Maximum operating distance	1000 m
Maximum pitch angular velocity	50 °/sec
Operating temperature (T-T)	-5 - 40 °C
Transmitter power consumption	100 mW
Built-in processor	-
Moving control functions	Backward, Forward, Turn left, Turn right, Upward

Weight and Dimensions

Depth	817 mm
Width	768 mm
Height	160 mm
Weight	1200 g
Rotor diameter	203.2 mm